at the inner panel forms a portion of the fan air duct and the outer panel forms a portion of the outer surface of the nacelle, and an open position whereat the vanes define passageways adapted to reverse fan air flow i.e., direct fan air flow back toward the front of the engine. ...
发明名称: Jet engine thrust reversers 发明人: KERRY THOMAS HENRY;WARD PETER ARTHUR 申请人: 申请日期: 1961-02-13 申请公布日期: 1963-08-08 代理机构: 代理人: 地址: 摘要: 二、法律状态 暂无信息 三、权利要求 暂无信息 四、说明书暂无信息 打开APP,查看更多专利的权利要求、说明书更多...
A jet engine (3) has streamlined casing (6) housing a cylinder (17) which is connected via a scissors link (13) to a pair of shutters (10, 12). In the normal position these are flat against the casing. For reverse thrust the cylinder (17) moves rearwards displacing the shutter (10...
Production of a downwardly and forwardly directed reverse thrust discharged from a reverse-thrust duct is controlled .Iadd.during landing . Iaddend.by a door in the rearward-discharge duct having its rearward portion pivotally mounted for swinging of its forward portion between a position lodged...
Turbojet engine thrust reverser having hinged doors A thrust reverser is disclosed for a turbojet engine having a cowling forming an outer boundary of a gas flow duct through which pressurized gases flow, the cowling having a reverse thrust opening, in which the thrust reverser comprises ... PA...
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The thrust reversal system is mounted in the housing surrounding the engine which forms an annular channel (C) for a pulsed gas flow. It comprises hinged flaps (14) located in apertures in the engine housing between forward (9) and aft (10) fixed members and lengthwise side members. The ...
A thrust reverser for a turbojet engine nacelle includes thrust reversal cascade vanes arranged about an annular flow duct having a stationary front casing, at least one movable cover moving backwards into a thrust reversal open position, and tilting flaps connected by rear pivots to the movable ...